A review of regenerative cooling technologies for scramjets

S Luo, D Xu, J Song, J Liu - Applied Thermal Engineering, 2021 - Elsevier
Regenerative cooling technologies are considered as an effective and realizable thermal
protection method in scramjets. In this paper, a review of regenerative cooling on the …

Data-driven physical fields reconstruction of supercritical-pressure flow in regenerative cooling channel using pod-ae reduced-order model

W Jiang, T Pan, G Jiang, Z Sun, H Liu, Z Zhou… - International Journal of …, 2023 - Elsevier
In order to effectively estimate the physical fields of active cooling channel with supercritical
pressure hydrocarbon fuel, a novel data-driven reduced-order model framework is firstly …

Fluid-thermo-structural response of actively cooled scramjet combustor in hypersonic accelerating-cruise flight

NK Gopinath, KV Govindarajan… - International Journal of …, 2022 - Elsevier
This paper presents a three-dimensional transient fluid-thermo-structural study of an actively
cooled sandwich panel under hypersonic accelerating-cruise flight conditions. The thermo …

Numerical simulation of thermal insulation and longevity performance in new lightweight ladle

Y Sun, J Tian, D Jiang, B Tao, Y Liu… - Concurrency and …, 2020 - Wiley Online Library
For meeting the comprehensive requirements of “super insulation,”“lightweight,” and
“longevity” of the contemporary ladle, this article designs a new kind of lightweight ladle with …

[HTML][HTML] Analysis and optimization of flow and heat transfer performance of active thermal protection channel for hypersonic aircraft

Y Qiao, P Liu, W Liu, Z Liu - Case Studies in Thermal Engineering, 2022 - Elsevier
This paper presents a numerical simulation on the thermal–hydraulic performance of
multiple parallel cooling channels to realize active thermal protection of hypersonic aircraft …

Thermal protection system and thermal management for combined-cycle engine: Review and prospects

Y Dong, E Wang, Y You, C Yin, Z Wu - Energies, 2019 - mdpi.com
Combined-cycle engine is a potential propulsion system for hypersonic aircraft. To ensure
long-term, normal operation of combined-cycle engine under the harsh environment of high …

Prediction of thermochemical and transport properties of hydrocarbon aviation fuel in supercritical state with thermal decomposition

JS Kim, J Seo, D Han, KH Kim - Fuel, 2022 - Elsevier
A program was developed to predict the physical properties of hydrocarbon aviation fuel that
flows in regenerative cooling channels used for scramjet vehicles. The developed program …

The flow rate distribution of hydrocarbon fuel in parallel channels with different cross section shapes

Y Jiang, Y Xu, J Qin, S Zhang, K Chetehouna… - Applied Thermal …, 2018 - Elsevier
When pursuing higher flight Mach number, engine cooling arises to become more and more
important in advanced aero-engines. Taking the regenerative cooling of SCRamjet for …

Effect of geometry parameters on the hydrocarbon fuel flow rate distribution in pyrolysis zone of SCRamjet cooling channels

Y Jiang, J Qin, K Chetehouna, N Gascoin… - International Journal of …, 2019 - Elsevier
Hypersonic air-breathing propulsion (> Mach 5) based on SCRamjet promotes the
revolutions of both military and civilian applications. However, the engine thermal protection …

Thermal performance evaluation of a distributed regenerative cooling system using supercritical catalytic steam reforming of aviation kerosene for scramjet engine

S Liu, L Han, Q Cheng, P Wang, Y Zhang, F Li, L Liu - Energy, 2023 - Elsevier
Regenerative cooling technology plays an important role for development of scramjet
engine. In order to further improve thermal performance of regenerative cooling system with …